Composite structure

Details Composite structure Composite structure

1977-02-03

1978-10-17

Lesmes, George F.

Stock material or miscellaneous articles

Plural parts with edges or temporary joining means each...

523091, 5230913, 52726, 244119, 244131, 244132, 244133, 403268, 403270, 403293, 403377, 428 35, 428113, 428166, 428172, 428188, 428232, 428246, 428285, 428286, 428542, 428902, B32B 1906

Patent

active

041209982

ABSTRACT:
A composite structure capable of withstanding multidirectional stress loads in general and in particular high tension and compression loads transmitted to an aircraft center fuselage by wing loading. The structure is essentially a beam formed by inserting two stepped metal end caps into the ends of a graphite/epoxy B-staged tubular strut and subsequently laying-up multidirectional and unidirectional fibers to provide a structure which is in turn cocured and results in a unitized composite wing trunnion structure.

REFERENCES:
patent: 3080268 (1963-03-01), Bjork
patent: 3780969 (1973-12-01), Nussbaum et al.
patent: 3946127 (1976-03-01), Eisenmann et al.
patent: 3959544 (1976-05-01), Rogers
patent: 3978256 (1976-08-01), James
patent: 4012549 (1977-03-01), Slysh
patent: 4020202 (1977-04-01), Kreff

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